Stability of the Laminar Boundary Layer on a Blunted Plate in Supersonic Flow-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Stability of the Laminar Boundary Layer on a Blunted Plate in Supersonic Flow

Published:1980 Issue: Volume: Page:186-200
ISSN:
Container-title:Laminar-Turbulent Transition
language:
Short-container-title:

Author:

Reshotko E.,Khan M. M. S.

Publisher

Springer Berlin Heidelberg

Link

http://link.springer.com/content/pdf/10.1007/978-3-642-81485-3_18.pdf

Reference13 articles.

1. NACA Report;WE Moeckel,1957

2. NASA TN;PF Brinich,1956

3. Stetson, K.F. and Rushton, G.H.; Shock Tunnel Investigation of Boundary Layer Transition at M = 5.5, AIAA Journal, Vol. 5, No, 5, May 1967.

4. AIAA Paper;KF Stetson,1979

5. NASA TN D-1071;DW Jillie,1961

Cited by 14 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical Investigation of Hypersonic Boundary-Layer Transition for an Ogive Cone;AIAA SCITECH 2022 Forum;2022-01-03

2. Direct Numerical Simulations of laminar-turbulent boundary-layer transition for blunt cones at Mach 6: Effect of Varying Nose Bluntness;AIAA AVIATION 2021 FORUM;2021-07-28

3. Effects of Nose Bluntness on Hypersonic Boundary-Layer Receptivity and Stability;Journal of Spacecraft and Rockets;2021-05

4. Direct Numerical Simulations of laminar-turbulent boundary-layer transition for a blunt cone at Mach 6;AIAA Scitech 2021 Forum;2021-01-04

5. Influence of the Entropy Layer on Turbulence Transition of the Supersonic Boundary Layer in the Wake with Isolated Roughnesses;Fluid Dynamics;2020-09

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线，采集、加工和组织学术论文而形成的新型学术文献查询和分析系统，可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容，当前同舟云学术共收录了国内外主流学术期刊6万余种，收集的期刊论文及会议论文总量共计约1.5亿篇，并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询！咨询电话：010-8811{复制后删除}0370

www.globalauthorid.com

TOP